The present invention relates to a multi-copter carrying apparatus(100). The present invention includes a handle(102), a casing(104), a sensor(106), an antenna(108), and a base(110). The sensor(106) is assembled inside the casing(104). The antenna(108) is assembled inside the casing(104). The multi-copter carrying ...

The present invention relates to a multi-copter stability system(100). The present invention includes a multi-copter(122), a payload connector(104), a multi-copter chassis(106), a drive unit(108), a point of center of gravity(110), a rail system(102), a battery unit(112), a sensor(114), a control computer(116) and a...

The present invention relates to a flexible configuration multi-copter drive system(100). The present invention includes a drive unit(102), a mounting rail(118), one or more rotating drives(104), a main multi-copter body(116), a drive unit socket(106), an electronic motor control(108), a control unit(110), a pluggab...